What was found
LOWER EXTERIOR FUSELAGE, AT LAV VENT, SKIN IS CORRODED BETWEEN VENT TUBE AND INTERIOR SKIN. GROUNDED - YES. REMOVED CORROSION FROM LOWER SKIN AT LAV VENT, ORIGINAL THICKNESS 0.125", WITH 0.005" REMOVED, AND 0.120" REMAINING, FOUND TO BE WITHIN LIMITS IAW B737-800 SRM 53-00-01-1A-1. ALODINED, PRIMED AND PAINTED AREA IAW B737-800 SRM 53-00-01-1A-1, AND B737-800 AMM 51-21-72.T.8224B